Auxiliary gas turbine engine assembly, aircraft component...

Details Auxiliary gas turbine engine assembly, aircraft component... Auxiliary gas turbine engine assembly, aircraft component...

B - Operations, Transporting

64

D

B64D 41/00 (2006.01) B64D 13/00 (2006.01) B64D 33/02 (2006.01) F01D 13/02 (2006.01) F02C 7/04 (2006.01)

Patent

CA 2581822

A non-aircraft-propelling auxiliary gas turbine engine assembly (10) includes an auxiliary gas turbine engine (12) and a mixing damper (14). The auxiliary engine and the mixing damper are installable in an aircraft (16) having at least one aircraft--propelling main gas turbine engine (18). The auxiliary engine includes a compressor (20) having a compressor inlet (22). The mixing damper has first and second inlets (24 and 26) and has an outlet (28). The outlet is fluidly connectable to the compressor inlet. The first and second inlets are adapted to receive first and second gas streams (30 and 32) which have been compressed by at least one main engine.

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